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西北工业大学 国内
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Theoretical study of the flame describing function of AP/HTPB propellant flame based on sandwich model
Guanyu Xu,
Peijin Liu
,
Wen Ao
, Bingning Jin
航天学院
Northwestern Polytechnical University Xian
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Engineering
Acoustic Oscillation
100%
Theoretical Study
100%
Forcing Frequency
75%
Forcing Amplitude
75%
Acoustic Mode
25%
Heat Flux
25%
Nonlinearity
25%
Rocket Engine
25%
Longitudinal Mode
25%
Physics
Polybutadiene
100%
Rocket Engine
50%
Composite Propellant
50%
Propellant Combustion
50%
Earth and Planetary Sciences
Propellant Combustion
50%